Ten-ampere-level, applied-field-dominant operation in magnetoplasmadynamic thrusters D Ichihara, T Uno, H Kataoka, J Jeong, A Iwakawa, A Sasoh Journal of Propulsion and Power 33 (2), 360-369, 2017 | 32 | 2017 |
Anode geometry effects on ion beam energy performance in helicon electrostatic thruster A Uchigashima, T Baba, D Ichihara, A Iwakawa, A Sasoh, T Yamazaki, ... IEEE Transactions on Plasma Science 44 (3), 306-313, 2016 | 13 | 2016 |
Electrostatic-magnetic-hybrid thrust generation in central–cathode electrostatic thruster (CC–EST) A Sasoh, H Kasuga, Y Nakagawa, T Matsuba, D Ichihara, A Iwakawa Acta Astronautica 152, 137-145, 2018 | 11 | 2018 |
Electrostatic ion acceleration across a diverging magnetic field D Ichihara, A Uchigashima, A Iwakawa, A Sasoh Applied Physics Letters 109 (5), 2016 | 11 | 2016 |
Electrostatic–magnetic hybrid ion acceleration for high-thrust-density operation D Ichihara, R Nakano, Y Nakamura, K Kinefuchi, A Sasoh Journal of Applied Physics 130 (22), 2021 | 9 | 2021 |
Modelling of a 1 T high-temperature superconducting applied field module for a magnetoplasmadynamic thruster JR Olatunji, NM Strickland, MRG Winchester, K Kinefuchi, D Ichihara, ... TENCON 2021-2021 IEEE Region 10 Conference (TENCON), 173-178, 2021 | 9 | 2021 |
Effects of magnetic field profile near anode on ion acceleration characteristics of a diverging magnetic field electrostatic thruster D Ichihara, A Iwakawa, A Sasoh Journal of Applied Physics 122 (4), 2017 | 8 | 2017 |
Energy conversion efficiency of electrical exploding foil accelerators D Ichihara, G Fukushima, D Kuwabara, A Sasoh AIP Advances 11 (9), 2021 | 5 | 2021 |
Operation characteristics of steady-state, applied field, rectangular magnetoplasmadynamics (MPD) thruster D Ichihara, S Harada, H Kataoka, S Yokota, A Sasoh Journal of the Japan Society for Aeronautical and Space Sciences 63 (2), 37-44, 2015 | 5 | 2015 |
Steady-state, applied-field, rectangular magnetoplasmadynamics thruster using hollow cathode A Sasoh, D Ichihara, T Enoki, S Yokota 48th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit, 4276, 2012 | 5 | 2012 |
Numerical and experimental study on the behavior of vortex rings generated by shock–bubble interaction K Kitamura, Z Yue, T Fujimoto, H Asai, A Kubota, M Myokan, D Ichihara, ... Physics of Fluids 34 (4), 2022 | 3 | 2022 |
Thrust Density Enhancement in an Electrostatic–Magnetic Hybrid Thruster D Ichihara, K Oka, A Higo, Y Nakamura, K Kinefuchi, A Sasoh Journal of Propulsion and Power 37 (6), 973-976, 2021 | 3 | 2021 |
High-specific-impulse electrostatic thruster with argon propellant D Ichihara, T Matsuba, A Iwakawa, A Sasoh Journal of Propulsion and Power 36 (2), 256-263, 2020 | 3 | 2020 |
Central and external cathode operations in a diverging-magnetic-field electrostatic thruster D Ichihara, Y Nakagawa, A Iwakawa, A Sasoh Journal of Propulsion and Power 36 (1), 68-77, 2020 | 3 | 2020 |
Steady-state, applied-field, rectangular MPD thrusters S Yokota, D Ichihara, H Kataoka, S Harada, A Sasoh IEPC Paper 246, 2013, 2013 | 3 | 2013 |
Energetic ion and plasma oscillation measurements during plume mode operation of a hollow cathode A Suzuki, K Kinefuchi, D Ichihara, S Cho, H Watanabe, K Kubota Physics of Plasmas 30 (7), 2023 | 2 | 2023 |
Similar Thrust Performance in Diverging-Magnetic-Field Electrostatic Thruster with Monoatomic Propellants D Ichihara, A Sasoh Journal of Propulsion and Power 35 (1), 236-238, 2019 | 2 | 2019 |
Ten-Ampere-Level, Direct Current Operation of Applied-Field Magnetoplasmadynamics (MPD) Thruster using LaB6 Hollow Cathode H Kasuga, K Mizutani, D Ichihara, A Iwakawa, A Sasoh, K Kojima, ... 35th International Electric Propulsion Conference, 2017 | 2 | 2017 |
Power matching between plasma generation and electrostatic acceleration in helicon electrostatic thruster D Ichihara, Y Nakagawa, A Uchigashima, A Iwakawa, A Sasoh, ... Acta Astronautica 139, 157-164, 2017 | 2 | 2017 |
定常作動同軸 AF-MPD の電極形状が推進性能に及ぼす影響 鵜生, 知輝, 片岡, 久志, 鄭栽勲, 市原, 岩川, 輝,佐宗, 章弘 平成 26 年度宇宙輸送シンポジウム: 講演集録= Proceedings of Space …, 2015 | 2 | 2015 |